GB130859A - Improvements in Aeroplanes. - Google Patents

Improvements in Aeroplanes.

Info

Publication number
GB130859A
GB130859A GB18035/18A GB1803518A GB130859A GB 130859 A GB130859 A GB 130859A GB 18035/18 A GB18035/18 A GB 18035/18A GB 1803518 A GB1803518 A GB 1803518A GB 130859 A GB130859 A GB 130859A
Authority
GB
United Kingdom
Prior art keywords
plane
planes
main
aspect ratio
auxiliary
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB18035/18A
Inventor
Alfred Guillermo Leigh
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB18035/18A priority Critical patent/GB130859A/en
Publication of GB130859A publication Critical patent/GB130859A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/08—Aircraft not otherwise provided for having multiple wings

Abstract

130,859. Leigh, A. G. Nov. 4, 1918. Planes, arrangement and disposition of. - Aeroplanes with a main plane 10, Fig. 8, of normal or low aspect ratio have an auxiliary plane 20 of high aspect ratio below and in front of the main plane 10, the horizontal distance between the front edge 25 of the plane 10 and the rear edge 23 of the plane 20 never exceeding the chord of the plane 20. The centre of gravity 28, Fig. 7, lies below the planes, and between the vertical transverse planes passing through the centres of pressure 34, 35 of the main and auxiliary planes 10, 20. Rigid stabilizing-planes 36, 37, Fig. 1, extend from the junctions 21, 22 of the planes 10, 20. The inner end portions of the plane 10 curve down to meet the fuselage 11 in walls 14, windows being provided opposite the seats of the pilot and passenger, and stream-line bars 12 bridging the gap in the plane 10.
GB18035/18A 1918-11-04 1918-11-04 Improvements in Aeroplanes. Expired GB130859A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB18035/18A GB130859A (en) 1918-11-04 1918-11-04 Improvements in Aeroplanes.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18035/18A GB130859A (en) 1918-11-04 1918-11-04 Improvements in Aeroplanes.

Publications (1)

Publication Number Publication Date
GB130859A true GB130859A (en) 1919-08-14

Family

ID=32347814

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18035/18A Expired GB130859A (en) 1918-11-04 1918-11-04 Improvements in Aeroplanes.

Country Status (1)

Country Link
GB (1) GB130859A (en)

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